Directory

 

 
 
General InformationPublications

  • Shane Haydt, Stephen Lynch and Scott Lewis, 2017, "The effect of area ratio change via increased hole length for shaped film cooling holes with constant expansion angles"
  • Shane Haydt, Stephen Lynch and Scott Lewis, 2017, "The effect of meter-diffuser offset in shaped film cooling holes", ASME J. Turbomachinery
  • Stephen Lynch and Karen A Thole, 2017, "Heat transfer and film cooling on a contoured blade endwall with platform gap leakage", ASME J. Turbomachinery, 139, (5)
  • Stephen Lynch, 2017, "Measurements and predictions of the three-dimensional boundary layer in a turbine blade passage", AIAA Journal of Propulsion and Power
  • Kirsten Muirhead and Stephen Lynch, 2017, "A computational study of combustor dilution flow interaction with turbine vanes", AIAA SciTech
  • David Saltzman, Michael Bichnevicius, Stephen Lynch, Timothy W Simpson, Edward Reutzel, Corey Dickman and Richard Martukanitz, 2017, "Experimental comparison of a traditionally built versus additively manufactured aircraft heat exchanger", AIAA SciTech
  • Michael Leonetti, Stephen Lynch, Jacqueline O'Connor and Sean Bradshaw, 2017, "Combustor dilution hole placement and its effect on the turbine inlet flowfield", Journal of Propulsion and Power
  • Shawn Siroka, Melissa Shallcross and Stephen Lynch, 2016, "Unsteady heat transfer around low aspect ratio cylinders in an array", ASME IMECE
  • Eric Lange, Stephen Lynch and Scott Lewis, 2016, "Computational and experimental studies of the effect of midpassage gap misalignment on a contoured turbine blade endwall", ASME International Gas Turbine Institute Turbo Expo
  • Shane Haydt, Stephen Lynch and Scott Lewis, 2016, "The effect of meter-diffuser offset in shaped film cooling holes"
  • Stephen Lynch and Karen A Thole, 2016, "Comparison of the three-dimensional boundary layer on flat versus contoured turbine endwalls", ASME J. Turbomachinery, 138, (4)
  • Stephen Lynch, 2016, "Measurements and predictions of the three-dimensional boundary layer in a turbine blade passage"
  • Corey Anderson and Stephen Lynch, 2016, "Time resolved stereo-PIV measurements of the horseshoe vortex system at multiple locations in a low aspect ratio pin-fin array", Experiments in Fluids, 57, (5)
  • Corey Anderson and Stephen Lynch, 2015, "Time-resolved stereo-PIV measurements of the horseshoe vortex system in pin fin arrays"
  • Stephen Lynch and Karen A Thole, 2015, "Comparison of the three-dimensional boundary layer on flat versus contoured turbine endwalls"
  • Stephen Lynch and Karen A Thole, 2015, "Heat transfer and film cooling on a contoured blade endwall with platform gap leakage"
  • I Milanovic, J Whiton, R Florea, Stephen Lynch, G Tillman and M Stucky, 2014, "RANS simulations for sensitivity analysis of compressor transition duct"
  • Stephen Lynch, K A Thole, A Kohli, C Lehane and T Praisner, 2013, "Endwall heat transfer for a turbine blade with an upstream cavity and rim seal leakage"
  • Seth A Lawson, S P Lynch and K A Thole, 2013, "Simulations of multi-phase particle deposition on a non-axisymmetric contoured endwall with film cooling", ASME J. of Turbomachinery, 35, pp. 11
  • Stephen Lynch, K A Thole, A Kohli, C Lehane and T Praisner, 2013, "Aerodynamic loss for a turbine blade with endwall leakage features and contouring"
  • S A Lawson, Stephen Lynch and K A Thole, 2012, "Simulations of multi-phase particle deposition on a non-axisymmetric contoured endwall with film cooling"
  • Stephen Lynch, K A Thole, A Kohli and C Lehane, 2011, "Computational predictions of heat transfer and film cooling for a turbine blade with non-axisymmetric endwall contouring", ASME J. of Turbomachinery, 133, pp. 9
  • Stephen Lynch, S Narayan, K A Thole, A Kohli and C Lehane, 2011, "Heat transfer for a turbine blade with non-axisymmetric endwall contouring", ASME J. of Turbomachinery, 133, pp. 8
  • Stephen Lynch and K A Thole, 2011, "The effect of the combustor-turbine slot and mid-passage gap on vane endwall heat transfer", ASME J. of Turbomachinery, 133, pp. 8
  • Stephen Lynch, K A Thole, A Kohli and C Lehane, 2010, "Computational predictions of heat transfer and film cooling for a turbine blade with non-axisymmetric endwall contouring"
  • Stephen Lynch and K A Thole, 2009, "The effect of the combustor-turbine slot and mid-passage gap on vane endwall heat transfer"
  • Stephen Lynch, S Narayan, K A Thole, A Kohli and C Lehane, 2009, "Heat transfer for a turbine blade with non-axisymmetric endwall contouring"
  • Stephen Lynch and K A Thole, 2008, "The effect of combustor-turbine interface gap leakage on the endwall heat transfer for a nozzle guide vane", ASME J. Turbomachinery, 130, pp. 9
  • Stephen Lynch and K A Thole, 2007, "The effect of combustor-turbine interface gap leakage on the endwall heat transfer for a nozzle guide vane"
 

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The Department of Mechanical and Nuclear Engineering at Penn State is one of the nation’s largest and most successful engineering departments. We serve more than 1,000 undergraduate students and more than 330 graduate students

We offer B.S. degrees in mechanical engineering and nuclear engineering as well as resident (M.S., Ph.D.) and online (M.S., M.Eng.) graduate degrees in nuclear engineering and mechanical engineering. MNE's strength is in offering hands-on experience in highly relevant research areas, such as energy, homeland security, biomedical devices, and transportation systems.

Department of Mechanical and Nuclear Engineering

137 Reber Building

The Pennsylvania State University

University Park, PA 16802-4400

Phone: 814-865-2519